Inverse design of supercritical nozzles and cascades

DOI10.1002/NME.1620220209zbMath0591.76101OpenAlexW2087814974WikidataQ59893406 ScholiaQ59893406MaRDI QIDQ3720145

No author found.

Publication date: 1986

Published in: International Journal for Numerical Methods in Engineering (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1002/nme.1620220209

zbMATH Keywords

turbine cascadesupercritical compressor cascadecascade geometryautomatic tuning of the upstream boundary distributionsboundary- layer calculationhigh resolution of steep gradientsinverse design of supercritical cascadeslocal mesh refinement with emboxed regionsNACA bladessupercritical nozzle flowthree-stage axial compressor

Mathematics Subject Classification ID

Transonic flows (76H05) Basic methods in fluid mechanics (76M99)

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